Turbine rotor blade airfoil profile

ABSTRACT

The present application provides a turbine rotor blade including an airfoil shape and a trailing edge shape. The airfoil shape may have a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I, while the trailing edge profile is defined by Table II. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a height of the airfoil in the unit of distance (e.g., inches). The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z. The airfoil profile sections at Z distances may be joined smoothly with one another to form a complete airfoil shape.

FIELD

The present disclosure relates to an airfoil for a turbine rotor blade of a stage of a turbine and, more particularly, relates to a shape defining a profile for an airfoil of a turbine rotor blade.

BACKGROUND

Some jet aircraft and simple cycle or combined cycle power plant systems employ turbines, or so-called turbomachines, in their design and operation. Some of these turbines employ airfoils (e.g., stator vanes or nozzles and rotor blades), which during operation are exposed to fluid flows. These airfoils are configured to aerodynamically interact with the fluid flows and to generate energy from these fluid flows as part of power generation. For example, the airfoils may be used to create thrust, to convert kinetic energy to mechanical energy, and/or to convert thermal energy to mechanical energy. As a result of this interaction and conversion, the aerodynamic characteristics of these airfoils may result in losses that have an impact on system and turbine operation, performance, thrust, efficiency, and power.

BRIEF DESCRIPTION

Aspects and advantages of the turbine rotor blades in accordance with the present disclosure will be set forth in part in the following description, or may be obvious from the description, or may be learned through practice of the technology.

In accordance with one embodiment, the present application provides a turbine rotor blade including an airfoil shape. The airfoil shape may have a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a height of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z. The airfoil profile sections at Z distances may be joined smoothly with one another to form a complete airfoil shape.

In accordance with another embodiment, the present application provides a turbine rotor blade including an airfoil having an uncoated nominal suction-side profile substantially in accordance with suction-side Cartesian coordinate values of X, Y and Z set forth in Table I. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a height of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define suction-side profile sections at each Z distance. The suction-side profile sections at the Z distances may be joined smoothly with one another to form a complete (uncoated) suction-side nominal shape.

In accordance with another embodiment, the present application provides a turbine rotor blade that includes an airfoil having an uncoated nominal trailing edge profile substantially in accordance with Cartesian coordinate values of X. Y and Z set forth in Table II. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a height of the airfoil in the unit of distance. The X and Y when connected by smooth continuing arcs, define trailing edge profile sections at each Z distance. The trailing edge profile sections at the Z distances may be joined smoothly with one another to form a complete airfoil trailing edge shape.

These and other features, aspects and advantages of the present turbine rotor blades will become better understood with reference to the following description and appended claims. The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments of the technology and, together with the description, serve to explain the principles of the technology.

BRIEF DESCRIPTION OF THE DRAWINGS

A full and enabling disclosure of the present turbine rotor blades, including the best mode of making and using the present systems and methods, directed to one of ordinary skill in the art, is set forth in the specification, which makes reference to the appended figures, in which:

FIG. 1 is a schematic representation of an exemplary turbine having multiple stages with each stage including alternating rows of turbine rotor blades and stationary vanes or nozzles, according to at least one embodiment of the present disclosure; and

FIG. 2 is a perspective view of a turbine rotor blade, according to at least one embodiment of the present disclosure;

FIG. 3 provides a cross-sectional view of an airfoil portion of the turbine rotor blade of FIG. 2; and

FIG. 4 is an enlarged view of a trailing edge of the airfoil portion shown in FIG. 3.

DETAILED DESCRIPTION

Reference now will be made in detail to embodiments of the present turbine rotor blades, one or more examples of which are illustrated in the drawings. Each example is provided by way of explanation, rather than limitation of, the technology. In fact, it will be apparent to those skilled in the art that various modifications and variations can be made in the present technology without departing from the scope or spirit of the claimed technology. For instance, features illustrated or described as part of one embodiment can be used with another embodiment to yield a still further embodiment. Thus, it is intended that the present disclosure covers such modifications and variations as come within the scope of the appended claims and their equivalents.

The detailed description uses numerical and letter designations to refer to features in the drawings. Like or similar designations in the drawings and description have been used to refer to like or similar parts of the invention. As used herein, the terms “first”, “second”, and “third” may be used interchangeably to distinguish one component from another and are not intended to signify location or importance of the individual components.

As used herein, the terms “upstream” (or “forward”) and “downstream” (or “aft”) refer to the relative direction with respect to fluid flow in a fluid pathway. For example, “upstream” refers to the direction from which the fluid flows, and “downstream” refers to the direction to which the fluid flows.

It is sometimes necessary to describe parts that are disposed at differing radial positions with regard to a center axis. The term “radially” refers to the relative direction (i.e., movement or position) that is substantially perpendicular to an axial centerline of a particular component; the term “axially” refers to the relative direction (i.e., movement or position) that is substantially parallel and/or coaxially aligned to an axial centerline of a particular component; and the term “circumferentially” refers to the relative direction that extends around the axial centerline of a particular component.

Unless stated otherwise, terms of approximation, such as “generally,” or “about” include values within ten percent greater or less than the stated value. When used in the context of an angle or direction, such terms include within ten degrees greater or less than the stated angle or direction. For example, “generally vertical” includes directions within ten degrees of vertical in any direction, e.g., clockwise or counter-clockwise.

Referring now to the drawings, particularly to FIG. 1, an exemplary turbine 10 of a gas turbine 12 includes a plurality of turbine stages arranged in serial flow order. Each stage of the turbine includes a row of stationary turbine nozzles or vanes (e.g., nozzles 100) disposed axially adjacent to a corresponding rotating row of turbine rotor blades 50. Four stages are illustrated in FIG. 1. The exact number of stages of the turbine 10 is a choice of engineering design and may be more or less than the four stages illustrated in FIG. 1. The four stages are merely exemplary of one turbine design and are not intended to limit the presently claimed turbine rotor blade in any manner.

The first stage comprises a plurality of turbine nozzles or vanes 100 and a plurality of turbine rotor blades 150. The turbine nozzles 100 are mounted to a casing 16 of the turbine and are annularly arranged about an axis of a turbine rotor 14. The turbine rotor blades 150 are annularly arranged about and coupled to the turbine rotor 14. A second stage of the turbine 12 includes a plurality of turbine nozzles 200 annularly arranged about the axis of the turbine rotor 14 and a plurality of turbine rotor blades 250 annularly arranged about and coupled to the turbine rotor 14. The turbine nozzles 200 may be coupled to the casing 16 of the turbine 12.

As shown in FIG. 1, a third stage of the turbine 12 includes a plurality of turbine nozzles 300 annularly arranged about the axis of the turbine rotor 14 and a plurality of turbine rotor blades 350 annularly arranged about and coupled to the turbine rotor 14. The turbine nozzles 300 may be coupled to the casing 16 of the turbine 12. In particular embodiments, the turbine 12 includes a fourth stage which includes a plurality of turbine nozzles 400 annularly arranged about the axis of the turbine rotor 14 and a plurality of turbine rotor blades 450 annularly arranged about and coupled to the turbine rotor 14. The fourth stage turbine nozzles 400 may be coupled to the casing 16 of the turbine 12.

It will be appreciated that the turbine nozzles 100, 200, 300 and 400 and turbine rotor blades 150, 250, 350 and 450 are disposed or at least partially disposed within a hot gas path 18 of the turbine 12. The various stages of the turbine 10 at least partially define the hot gas path 18 through which combustion gases, as indicated by arrows 20, flow during operation of the gas turbine 12.

FIG. 2 provides a perspective view of an exemplary turbine rotor blade 50 as may be incorporated in any stage of the turbine 12. For example, in one embodiment the turbine rotor blade 50 as presented in Table I below is representative of a turbine rotor blade 250 of the plurality of turbine rotor blades 250 of the second stage.

As shown in FIGS. 2 and 3 collectively, the turbine rotor blade 50 includes an airfoil 52 having a pressure-side wall 54 and an opposing suction-side wall 56. The pressure-side wall 54 and the suction-side wall 56 meet or intersect at a leading edge 58 and a trailing edge 60 of the airfoil 52. A chord line 62 extends between the leading edge 58 and the trailing edge 60 such that pressure and suction-side walls 54, 56 can be said to extend in chord or chordwise between the leading edge 58 and the trailing edge 60.

As shown in FIG. 2, the airfoil 52 includes a root or first end 64, which intersects with and extends radially outwardly from a base or platform 66 of the turbine rotor blade 50. The airfoil 52 terminates radially at a second end or radial tip 68 of the airfoil 52. The pressure-side and suction-side walls 54, 56 can be said to extend in span or in a span-wise direction 70 between the root 64 and/or the platform 66 and the radial tip 68 of the airfoil 52. In other words, each turbine rotor blade 50 includes an airfoil 52 having opposing pressure-side and suction-side walls 54, 56 that extend in chord or chordwise 62 between opposing leading and trailing edges 58, 60 and that extend in span or span-wise 70 between the root 64 and the radial tip 68 of the airfoil 52.

In particular configurations, the airfoil 52 may include a fillet 72 formed between the platform 66 and the airfoil 52 proximate to the root 64. The fillet 72 can include a weld or braze fillet, which can be formed via conventional MIG welding, TIG welding, brazing, etc., and can include a profile that can reduce fluid dynamic losses as a result of the presence of fillet 72. In particular embodiments, the platform 66, the airfoil 52 and the fillet 72 can be formed as a single component, such as by casting and/or machining and/or 3D printing and/or any other suitable technique now known or later developed and/or discovered. In particular configurations, the turbine rotor blade 50 includes a mounting portion 74 (such as a dovetail joint), which is formed to connect and/or to secure the turbine rotor blade 50 to the rotor shaft 14.

The airfoil 52 of the turbine rotor blade 50 has a nominal profile at any cross-section taken between the platform 66 or the root 64 and the radial tip 68, e.g., the cross section shown in FIG. 3. As shown in FIG. 4, the airfoil 52 may further define a trailing edge profile 61 proximate the trailing edge 60. For example, in one embodiment Table II below is representative of the trailing edge profile 61 for a turbine rotor blade 250 of the plurality of turbine rotor blades 250. A “profile” is the range of variation between measured points on an airfoil surface and the ideal position listed in Table I or Table II. The actual profile on a manufactured turbine blade will be different from those in Table I or Table II (e.g., due to coatings), and the design is robust to this variation, meaning that mechanical and aerodynamic function are not impaired.

The X, Y, and Z values are given in Table I and Table II as percentage values of the airfoil height or span, as measured in any given unit of distance (e.g., inches). As one example only, the height or radial span of the airfoil 52 of turbine rotor blade 50 may be from about 5 inches to about 15 inches (about 13 centimeters to about 38 centimeters). However, it is to be understood that heights below or above this range may also be employed as desired in the specific application.

A gas turbine hot gas path requires airfoils that meet system requirements of aerodynamic and mechanical blade loading and efficiency. To define the airfoil shape of each turbine rotor blade airfoil, there is a unique set or loci of points in space that meet the stage requirements and that can be manufactured. This unique loci of points meet the requirements for stage efficiency and are arrived at by iteration between aerodynamic and mechanical loadings enabling the turbine to run in an efficient, safe and smooth manner. These points are unique and specific to the system.

The loci that define the turbine rotor blade airfoil profile include a set of about 2,400 points with X. Y and Z dimensions relative to a reference origin coordinate system. The Cartesian coordinate system of X, Y and Z values given in Table I below defines the profile of the turbine rotor blade airfoil at various locations along its height. Similarly, the loci that define the turbine rotor blade trailing edge profile include a set of about 700 points with X, Y, and Z dimensions relative to a reference origin coordinate system. The Cartesian coordinate system of X. Y and Z values given in Table II below defines the profile of the trailing edge of the turbine rotor blade airfoil at various locations along its height.

Table I and Table II list data for a uncoated airfoil at cold or room temperature. The envelope/tolerance for the coordinates is about +/−5% in a direction normal to any airfoil surface location and/or about +/−5% of the chord 62 in a direction nominal to any airfoil surface location. In other words, the airfoil layout, as embodied by the disclosure, is robust to this range of variation without impairment of mechanical and aerodynamic functions.

A point data origin 76 is defined at or proximate to the root 64 at the leading edge 58. In one embodiment as presented in Table I and Table II below, the point data origin 76 is defined at or proximate to (above or below) a transition or intersection line 78 defined between the fillet 72 and the airfoil 52. The point data origin 76 corresponds to the non-dimensional Z value of Table I and/or Table II (presented below) at Z equals 0.

The Cartesian coordinate values for the X, Y and Z coordinates are set forth in non-dimensionalized units provided in Table I and/or Table II, although other units of dimensions may be used when the values are appropriately converted. The X, Y and Z values set forth in Table I and/or Table II are expressed in non-dimensional form (X, Y, and Z) from 0% to 100% of the height or span of the airfoil 52. As one example only, the Cartesian coordinate values of X, Y and Z may be convertible to dimensional distances by multiplying the X, Y and Z values by a height of the airfoil at the leading edge 58 and multiplying by a constant number (e.g., 100). As one example only, the Cartesian coordinate values of X. Y and Z may be convertible to dimensional distances by multiplying the X, Y and Z values by a height of the airfoil at the trailing edge 60 and multiplying by a constant number (e.g., 100).

To convert the Z value to a Z coordinate value, e.g., in inches, the non-dimensional Z value given in Table I and/or Table II is multiplied by the Z height of the airfoil in inches. As described above, the Cartesian coordinate system has orthogonally-related X, Y and Z axes, and the X axis lies generally parallel to a centerline of the rotor shaft 14, i.e., the rotary axis, and a positive X coordinate value is axial toward an aft, i.e., exhaust end of the turbine 10. The positive Y coordinate value extends tangentially in the direction of rotation of the rotor and the positive Z coordinate value is radially outwardly from the base 66 toward the radial tip 68. All the values in Table I and/or Table II are given at room temperature and do not include the fillet 72 or coatings (not shown).

By defining X and Y coordinate values at selected locations in a Z direction normal to the X, Y plane, the profile section or airfoil shape of the airfoil 52 of the turbine rotor blade 50, at each Z distance along the length of the airfoil 52 can be ascertained. By connecting the X and Y values with smooth continuing arcs, each profile section at each distance Z is fixed. The airfoil profiles of the various surface locations between the distances Z are determined by smoothly connecting the adjacent profile sections to one another to form the airfoil profile.

The Table I values are generated and shown to four decimal places for determining the profile of the airfoil 52. Similarly, the Table II values are generated and shown to four decimal places for determining the trailing edge profile 61 of airfoil 52. As the turbine rotor blade 50 heats up during operation of the gas turbine 12, surface stress and temperature will cause a change in the X, Y and Z values. Accordingly, the values for the profile given in Table I and/or Table II define the “nominal” airfoil profile, that is, the profile of an uncoated airfoil at ambient, non-operating or non-hot conditions (e.g., room temperature).

There are typical manufacturing tolerances as well as coatings which must be accounted for in the actual profile of the airfoil 52. Each cross-section is joined smoothly with the other cross-sections to form the complete airfoil shape. It will therefore be appreciated that +/− typical manufacturing tolerances, i.e., +/− values, including any coating thicknesses, are additive to the X and Y values given in Table I and/or Table II below. Accordingly, a distance of +/−5% in a direction normal to any surface location along the airfoil profile defines an airfoil profile envelope for this particular turbine rotor blade 50 airfoil design and turbine 12, i.e., a range of variation between measured points on the actual airfoil surface at nominal cold or room temperature and the ideal position of those points as given in Table I and Table II below at the same temperature. The data provided in Table I and/or Table II s scalable (i.e., by uniform geometric scaling), and the geometry pertains to all aerodynamic scales, at, above and/or below 3000 RPM. The design of the airfoil 52 for turbine rotor blade 50 is robust to this range of variation without impairment of mechanical and aerodynamic functions.

TABLE I SUCTION−SIDE PRESSURE−SIDE X (%) Y (%) Z (%) X (%) Y (%) Z (%) 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 −0.3159 0.7251 0.0000 0.4642 −0.4025 0.0000 −0.3072 1.5235 0.0000 1.0487 −0.6028 0.0000 −0.1329 2.2987 0.0000 1.6631 −0.6596 0.0000 0.1406 3.0450 0.0000 2.2794 −0.6298 0.0000 0.4834 3.7663 0.0000 2.8880 −0.5383 0.0000 0.8754 4.4606 0.0000 3.4851 −0.4006 0.0000 1.3029 5.1299 0.0000 4.0735 −0.2282 0.0000 1.7603 5.7770 0.0000 4.6541 −0.0270 0.0000 2.2457 6.4049 0.0000 5.2262 0.2032 0.0000 2.7542 7.0144 0.0000 5.7934 0.4545 0.0000 3.2838 7.6076 0.0000 6.3577 0.7117 0.0000 3.8298 8.1864 0.0000 6.9249 0.9611 0.0000 4.3903 8.7517 0.0000 7.4950 1.1999 0.0000 4.9613 9.3054 0.0000 8.0679 1.4291 0.0000 5.5430 9.8485 0.0000 8.6438 1.6477 0.0000 6.1314 10.3830 0.0000 9.2226 1.8566 0.0000 6.7265 10.9078 0.0000 9.8052 2.0560 0.0000 7.3293 11.4230 0.0000 10.3897 2.2467 0.0000 7.9408 11.9257 0.0000 10.9771 2.4267 0.0000 8.5620 12.4159 0.0000 11.5675 2.5982 0.0000 9.1918 12.8925 0.0000 12.1607 2.7609 0.0000 9.8312 13.3538 0.0000 12.7558 2.9131 0.0000 10.4822 13.8016 0.0000 13.3548 3.0575 0.0000 11.1437 14.2321 0.0000 13.9557 3.1914 0.0000 11.8198 14.6/161 0.0000 14.5604 3.3165 0.0000 12.5093 15.0410 0.0000 15.1671 3.4331 0.0000 13.2113 15.4156 0.0000 15.7767 3.5390 0.0000 13.9268 15.7661 0.0000 16.3892 3.6363 0.0000 14.6539 16.0916 0.0000 17.0045 3.7239 0.0000 15.3925 16.3892 0.0000 17.6218 3.8009 0.0000 16.1417 16.6569 0.0000 18.2400 3.8683 0.0000 16.9015 16.8918 0.0000 18.8573 3.9252 0.0000 17.6719 17.0941 0.0000 19.4746 3.9714 0.0000 18.4500 17.2597 0.0000 20.0919 4.0080 0.0000 19.2367 17.3878 0.0000 20.7082 4.0330 0.0000 20.0273 17.4773 0.0000 21.3245 4.0475 0.0000 20.8180 17.5265 0.0000 21.9408 4.0513 0.0000 21.6067 17.5361 0.0000 22.5562 4.0436 0.0000 22.3925 17.5043 0.0000 23.1715 4.0253 0.0000 23.1773 17.4311 0.0000 23.7869 3.9955 0.0000 23.9641 17.3175 0.0000 24.4013 3.9540 0.0000 24.7470 17.1644 0.0000 25.0156 3.9001 0.0000 25.5222 16.9727 0.0000 25.6300 3.8337 0.0000 26.2839 16.7455 0.0000 26.2435 3.7557 0.0000 27.0312 16.4835 0.0000 26.8569 3.6651 0.0000 27.7650 16.1889 0.0000 27.4694 3.5602 0.0000 28.4872 15.8643 0.0000 28.0818 3.4427 0.0000 29.1970 15.5100 0.0000 28.6914 3.3127 0.0000 29.8951 15.1276 0.0000 29.2961 3.1682 0.0000 30.5789 14.7203 0.0000 29.8961 3.0113 0.0000 31.2491 14.2889 0.0000 30.4912 2.8418 0.0000 31.9049 13.8372 0.0000 31.0806 2.6588 0.0000 32.5453 13.3663 0.0000 31.6651 2.4614 0.0000 33.1703 12.8791 0.0000 32.2448 2.2515 0.0000 33.7818 12.3754 0.0000 32.8188 2.0281 0.0000 34.3817 11.8564 0.0000 33.3879 1.7912 0.0000 34.9701 11.3229 0.0000 33.9522 1.5398 0.0000 35.5469 10.7759 0.0000 34.5098 1.2750 0.0000 36.1122 10.2154 0.0000 35.0635 0.9957 0.0000 36.6669 9.6444 0.0000 35.6115 0.7030 0.0000 37.2100 9.0637 0.0000 36.1536 0.3948 0.0000 37.7426 8.4734 0.0000 36.6890 0.0742 0.0000 38.2635 7.8754 0.0000 37.2158 −0.2590 0.0000 38.7739 7.2706 0.0000 37.7310 −0.6038 0.0000 39.2747 6.6581 0.0000 38.2375 −0.9601 0.0000 39.7648 6.0389 0.0000 38.7354 −1.3280 0.0000 40.2473 5.4130 0.0000 39.2236 −1.7064 0.0000 40.7201 4.7803 0.0000 39.7022 −2.0955 0.0000 41.1843 4.1418 0.0000 40.1731 −2.4951 0.0000 41.6417 3.4976 0.0000 40.6344 −2.9044 0.0000 42.0905 2.8466 0.0000 41.0880 −3.3242 0.0000 42.5334 2.1918 0.0000 41.5339 −3.7528 0.0000 42.9687 1.5312 0.0000 41.9711 −4.1919 0.0000 43.3972 0.8648 0.0000 42.4015 −4.6387 0.0000 43.8190 0.1945 0.0000 42.8243 −5.0952 0.0000 44.2360 −0.4796 0.0000 43.2393 −5.5603 0.0000 44.6472 −1.1585 0.0000 43.6467 −6.0312 0.0000 45.0526 −1.8403 0.0000 44.0453 −6.5089 0.0000 45.4523 −2.5259 0.0000 44.4344 −6.9932 0.0000 45.8481 −3.2145 0.0000 44.8148 −7.4834 0.0000 46.2381 −3.9059 0.0000 45.1874 −7.9803 0.0000 46.6242 −4.5993 0.0000 45.5515 −8.4830 0.0000 47.0065 −5.2955 0.0000 45.9078 −8.9915 0.0000 47.3840 −5.9937 0.0000 46.2583 −9.5038 0.0000 47.7596 −6.6928 0.0000 46.6011 −10.0219 0.0000 48.1313 −7.3939 0.0000 46.9382 −10.5448 0.0000 48.5001 −8.0959 0.0000 47.2694 −11.0715 0.0000 48.8670 −8.8008 0.0000 47.5959 −11.6021 0.0000 49.2291 −9.5067 0.0000 47.9185 −12.1337 0.0000 49.5864 −10.2154 0.0000 48.2401 −12.6672 0.0000 49.9379 −10.9280 0.0000 48.5608 −13.2007 0.0000 50.2826 −11.6435 0.0000 48.8834 −13.7342 0.0000 50.6206 −12.3619 0.0000 49.2060 −14.2667 0.0000 50.951.0 −13.0842 0.0000 49.5305 −14.7983 0.0000 51.2745 −13.8093 0.0000 49.8570 −15.3279 0.0000 51.5923 −14.5373 0.0000 50.1863 −15.8576 0.0000 51.9053 −15.2673 0.0000 50.5205 −16.3824 0.0000 52.2096 −16.0001 0.0000 50.8614 −16.9034 0.0000 52.5043 −16.7378 0.0000 51.2004 −17.4263 0.0000 52.5572 −16.8813 0.0000 51.2909 −17.5553 0.0000 52.6083 −17.0459 0.0000 51.3997 −17.6940 0.0000 52.6506 −17.2125 0.0000 51.5172 −17.8269 0.0000 52.6824 −17.3820 0.0000 51.6433 −17.9511 0.0000 52.6978 −17.5544 0.0000 51.7801 −18.0638 0.0000 52.6901 −17.7268 0.0000 51.9322 −18.1534 0.0000 52.6477 −17.8934 0.0000 52.0998 −18.2092 0.0000 52.5659 −18.0436 0.0000 52.2770 −18.2160 0.0000 52.4426 −18.1591 0.0000 52.4426 −18.1591 0.0000 0.0924 1.9915 9.9997 0.0924 1.9915 9.9997 −0.1965 2.7195 9.9997 0.5364 1.5755 9.9997 −0.1676 3.5014 9.2997 1.1017 1.3492 9.9997 0.0270 4.2612 9.9997 1.7045 1.2634 9.9997 0.3207 4.9912 9.9997 2.3102 1.2663 9.9997 0.6799 5.6884 9.9997 2.9150 1.3289 9.9997 1.0863 6.3567 9.9997 3.5101 1.4387 9.9997 1.5302 7.0010 9.9997 4.0946 1.5841 9.9997 2.0049 7.6250 9.9997 4.6724 1.7584 9.9997 2.5076 8.2278 9.9997 5.2425 1.9597 9.9997 3.0334 8.8114 9.9997 5.8068 2.1860 9.9997 3.5775 9.3767 9.9997 6.3673 2.4277 9.9997 4.1380 9.9246 9.9997 6.9287 2.6656 9.9997 4.7100 10.4571 9.9997 7.4940 2.8842 9.9997 5.2926 10.9781 9.9997 8.0631 3.0883 9.9997 5.8829 11.4866 9.9997 8.6352 3.2809 9.9997 6.4819 11.9873 9.9997 9.2091 3.4591 9.9997 7.0876 12.4775 9.9997 9.7869 3.6247 9.9997 7.7020 12.9571 9.9997 10.3676 3.7759 9.9997 8.3270 13.4260 9.9997 10.9511 3.9146 9.9997 8.9616 13.8806 9.9997 11.5376 4.0407 9.9997 9.6078 14.3216 9.9997 12.1270 4.1553 9.9997 10.2655 14.7473 9.9997 12.7182 4.2574 9.9997 10.9338 15.1565 9.9997 13.3124 4.3469 9.9997 11.6127 15.5465 9.9997 13.9095 4.4240 9.9997 12.3013 15.9144 9.9997 14.5094 4.4895 9.9997 12.9994 16.2592 9.9997 15.1122 4.5434 9.9997 13.7072 16.5798 9.9997 15.7170 4.5858 9.9997 14.4285 16.8735 9.9997 16.3246 4.6156 9.9997 15.1623 17.1413 9.9997 16.9352 4.6339 9.9997 15.9077 17.3782 9.9997 17.5467 4.6407 9.9997 16.6636 17.5813 9.9997 18.1572 4.6358 9.9997 17.4292 17.7499 9.9997 18.7649 4.6195 9.9997 18.2015 17.8818 9.9997 19.3706 4.5915 9.9997 18.9767 17.9742 9.9997 19.9744 4.5521 9.9997 19.7529 18.0263 9.9997 20.5772 4.5020 9.9997 20.5320 18.0388 9.9997 21.1772 4.4413 9.9997 21.3129 18.0080 9.9997 21.7761 4.3691 9.9997 22.0968 17.9357 9.9997 22.3732 4.2872 9.9997 22.8759 17.8231 9.9997 22.9674 4.1938 9.9997 23.6424 17.6699 9.9997 23.5606 4.0898 9.9997 24.3984 17.4802 9.9997 24.1518 3.9752 9.9997 25.1437 17.2530 9.9997 24.7412 3.8491 9.9997 25.8785 16.9901 9.9997 25.3296 3.7133 9.9997 26.6046 16.6935 9.9997 25.9151 3.5660 9.9997 27.3182 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18.1900 39.9998 9.2418 9.6559 39.9998 7.5450 18.5732 39.9998 9.8283 9.6790 39.9998 8.1941 18.9295 39.9998 10.4128 9.6838 39.9998 8.8566 19.2579 39.9998 10.9974 9.6713 39.9998 9.5327 19.5574 39.9998 11.5819 9.6415 39.9998 10.2231 19.8270 39.9998 12.1645 9.5943 39.9998 10.9271 20.0649 39.9998 12.7471 9.5307 39.9998 11.6455 20.2700 39.9998 13.3297 9.4508 39.9998 12.3667 20.4385 39.9998 13.9104 9.3564 39.9998 13.0919 20.5714 39.9998 14.4911 9.2457 39.9998 13.8209 20.6668 39.9998 15.0679 9.1205 39.9998 14.5527 20.7274 39.9998 15.6390 8.9828 39.9998 15.2885 20.7515 39.9998 16.2062 8.8316 39.9998 16.0271 20.7390 39.9998 16.7676 8.6689 39.9998 16.7695 20.6899 39.9998 17.3252 8.4936 39.9998 17.5101 20.6051 39.9998 17.8780 8.3077 39.9998 18.2420 20.4867 39.9998 18.4278 8.1113 39.9998 18.9652 20.3345 39.9998 18.9729 7.9042 39.9998 19.6787 20.1516 39.9998 19.5141 7.6866 39.9998 20.3846 19.9378 39.9998 20.0514 7.4593 39.9998 21.0818 19.6942 39.9998 20.5859 7.2234 39.9998 21.7713 19.4226 39.9998 21.1165 6.9778 39.9998 22.4522 19.1241 39.9998 21.6432 6.7246 39.9998 23.1224 18.7995 39.9998 22.1671 6.4617 39.9998 23.7782 18.4538 39.9998 22.6881 6.1911 39.9998 24.4205 18.0879 39.9998 23.2062 5.9128 39.9998 25.0513 17.7027 39.9998 23.7204 5.6268 39.9998 25.6686 17.2982 39.9998 24.2298 5.3340 39.9998 26.2752 16.8755 39.9998 24.7345 5.0364 39.9998 26.8704 16.4364 39.9998 25.2342 4.7321 39.9998 27.4559 15.9818 39.9998 25.7302 4.4230 39.9998 28.0317 15.5109 39.9998 26.2213 4.1072 39.9998 28.5951 15.0275 39.9998 26.7086 3.7874 39.9998 29.1469 14.5335 39.9998 27.1920 3.4620 39.9998 29.6852 14.0289 39.9998 27.6716 3.1317 39.9998 30.2139 13.5137 39.9998 28.1473 2.7965 39.9998 30.7310 12.9908 39.9998 28.6192 2.4576 39.9998 31.2375 12.4582 39.9998 29.0881 2.1138 39.9998 31.7344 11.9170 39.9998 29.5533 1.7652 39.9998 32.2227 11.3681 39.9998 30.0145 1.4127 39.9998 32.7013 10.8125 39.9998 30.4729 1.0554 39.9998 33.1722 10.2482 39.9998 30.9284 0.6953 39.9998 33.6344 9.6771 39.9998 31.3810 0.3303 39.9998 34.0890 9.1003 39.9998 31.8298 −0.0385 39.9998 34.5358 8.5157 39.9998 32.2756 −0.4112 39.9998 34.9759 7.9254 39.9998 32.7186 −0.7877 39.9998 35.4083 7.3303 39.9998 33.1587 −1.1671 39.9998 35.8349 6.7284 39.9998 33.5959 −1.5514 39.9998 36.2547 6.1208 39.9998 34.0312 −1.9385 39.9998 36.6679 5.5083 39.9998 34.4626 −2.3295 39.9998 37.0762 4.8920 39.9998 34.8911 −2.7233 39.9998 37.4777 4.2709 39.9998 35.3177 −3.1220 39.9998 37.8735 3.6459 39.9998 35.7405 −3.5226 39.9998 38.2626 3.0180 39.9998 36.1613 −3.9280 39.9998 38.6468 2.3873 39.9998 36.5793 −4.3364 39.9998 39.0262 1.7526 39.9998 36.9943 −4.7485 39.9998 39.3999 1.1151 39.9998 37.4065 −5.1636 39.9998 39.7687 0.4757 39.9998 37.8157 −5.5825 39.9998 40.1327 −0.1676 39.9998 38.2231 −6.0033 39.9998 40.4938 −0.8118 39.9998 38.6266 −6.4280 39.9998 40.8501 −1.4589 39.9998 39.0262 −6.8546 39.9998 41.2045 −2.1080 39.9998 39.4230 −7.2831 39.9998 41.5541 −2.7590 39.9998 39.8168 −7.7155 39.9998 41.9017 −3.4119 39.9998 40.2059 −8.1498 39.9998 42.2455 −4.0658 39.9998 40.5911 −8.5880 39.9998 42.5864 −4.7225 39.9998 40.9715 −9.0300 39.9998 42.9263 −5.3783 39.9998 41.3461 −9.4758 39.9998 43.2653 −6.0360 39.9998 41.7168 −9.9246 39.9998 43.6043 −6.6928 39.9998 42.0828 −10.3782 39.9998 43.9413 −7.3515 39.9998 42.4439 −10.8346 39.9998 44.2765 −8.0102 39.9998 42.8002 −11.2949 39.9998 44.6116 −8.6689 39.9998 43.1507 −11.7591 39.9998 44.9457 −9.3285 39.9998 43.4964 −12.2281 39.9998 45.2789 −9.9891 39.9998 43.8354 −12.7009 39.9998 45.6102 −10.6497 39.9998 44.1715 −13.1776 39.9998 45.9395 −11.3113 39.9998 44.5037 −13.6552 39.9998 46.2650 −11.9758 39.9998 44.8350 −14.1358 39.9998 46.3847 −12.6422 39.9998 45.1624 −14.6173 39.9998 46.8987 −13.3124 39.9998 45.4879 −15.1007 39.9998 47.2097 −13.9836 39.9998 45.8115 −15.5870 39.9998 47.3150 −14.6567 39.9998 46.1312 −16.0743 39.9998 47.8164 −15.3318 39.9998 46.4490 −16.5644 39.9998 48.1130 −16.0088 39.9998 46.7639 −17.0565 39.9998 48.4067 −16.6877 39.9998 47.0768 −17.5496 39.9998 48.6956 −17.3676 39.9998 47.3869 −18.0455 39.9998 48.7515 −17.5120 39.9998 47.4746 −18.1784 39.9998 48.8054 −17.6776 39.9998 47.5824 −18.3229 39.9998 48.8497 −17.8462 39.9998 47.6989 −18.4586 39.9998 48.8824 −18.0176 39.9998 47.8241 −18.5867 39.9998 48.8988 −18.1919 39.9998 47.9618 −18.7023 39.9998 48.8892 −18.3662 39.9998 48.1159 −18.7938 39.9998 48.8449 −18.5347 39.9998 48.2854 −18.8506 39.9998 48.7601 −18.6859 39.9998 48.4645 −18.8573 39.9998 48.6330 −18.8005 39.9998 48.6330 −18.8005 39.9998 1.0083 12.5025 50.0005 1.0083 12.5025 50.0005 0.8474 13.2113 50.0005 1.3520 12.0230 50.0005 0.9620 13.9268 50.0005 1.8403 11.6927 50.0005 1.2278 14.6057 50.0005 2.3959 11.4923 50.0005 1.5832 15.2384 50.0005 2.9718 11.3797 50.0005 1.9982 15.8297 50.0005 3.5592 11.3306 50.0005 2.4585 16.3882 50.0005 4.1476 11.3306 50.0005 2.9564 16.9188 50.0005 4.7331 11.3691 50.0005 3.4812 17.4196 50.0005 5.3148 11.4432 50.0005 4.0301 17.8962 50.0005 5.8954 11.5395 50.0005 4.5964 18.3479 50.0005 6.4752 11.6262 50.0005 5.1780 18.7755 50.0005 7.0558 11.6840 50.0005 5.7722 19.1799 50.0005 7.6365 11.7196 50.0005 6.3808 19.5622 50.0005 8.2182 11.7379 50.0005 7.0029 19.9195 50.0005 8.7989 11.7360 50.0005 7.6413 20.2517 50.0005 9.3805 11.7148 50.0005 8.2943 20.5570 50.0005 9.9622 11.6734 50.0005 8.9655 20.8334 50.0005 10.5448 11.6137 50.0005 9.6501 21.0770 50.0005 11.1254 11.5347 50.0005 10.3396 21.2869 50.0005 11.7013 11.4384 50.0005 11.0369 21.4603 50.0005 12.2724 11.3258 50.0005 11.7398 21.5970 50.0005 12.8376 11.1977 50.0005 12.4486 21.6981 50.0005 13.3991 11.0532 50.0005 13.1641 21.7617 50.0005 13.9547 10.8943 50.0005 13.8863 21.7887 50.0005 14.5065 10.7210 50.0005 14.6144 21.7771 50.0005 15.0545 10.5342 50.0005 15.3366 21.7280 50.0005 15.5985 10.3348 50.0005 16.0492 21.6432 50.0005 16.1378 10.1230 50.0005 16.7551 21.5248 50.0005 16.6742 9.8986 50.0005 17.4533 21.3726 50.0005 17.2067 9.6627 50.0005 18.1437 21.1897 50.0005 17.7354 9.4161 50.0005 18.8275 20.9759 50.0005 18.2603 9.1600 50.0005 19.5035 20.7323 50.0005 18.7783 8.8952 50.0005 20.1737 20.4617 50.0005 19.2897 8.6217 50.0005 20.8353 20.1641 50.0005 19.7962 8.3414 50.0005 21.4844 19.8444 50.0005 20.2979 8.0535 50.0005 22.1199 19.5035 50.0005 20.7949 7.7598 50.0005 22.7430 19.1433 50.0005 21.2860 7.4584 50.0005 23.3555 18.7639 50.0005 21.7733 7.1512 50.0005 23.9564 18.3681 50.0005 22.2567 6.8392 50.0005 24.5476 17.9550 50.0005 22.7353 6.5204 50.0005 25.1293 17.5265 50.0005 23.2100 6.1969 50.0005 25.7013 17.0825 50.0005 23.6819 5.8685 50.0005 26.2627 16.6261 50.0005 24.1499 5.5343 50.0005 26.8116 16.1600 50.0005 24.6141 5.1963 50.0005 27.3499 15.6833 50.0005 25.0754 4.8544 50.0005 27.8777 15.1970 50.0005 25.5337 4.5078 50.0005 28.3948 14.7020 50.0005 25.9892 4.1572 50.0005 28.9023 14.1974 50.0005 26.4418 3.8029 50.0005 29.4011 13.6851 50.0005 26.8916 3.4446 50.0005 29.8903 13.1651 50.0005 27.3393 3.0835 50.0005 30.3718 12.6373 50.0005 27.7843 2.7185 50.0005 30.8446 12.1019 50.0005 28.2263 2.3497 50.0005 31.3098 11.5598 50.0005 28.6664 1.9780 50.0005 31.7672 11.0099 50.0005 29.1045 1.6034 50.0005 32.2179 10.4542 50.0005 29.5398 1.2259 50.0005 32.6608 9.8919 50.0005 29.9741 0.8455 50.0005 33.0971 9.3237 50.0005 30.4055 0.4622 50.0005 33.5266 8.7488 50.0005 30.8350 0.0761 50.0005 33.9503 8.1691 50.0005 31.2626 −0.3130 50.0005 34.3673 7.5836 50.0005 31.6882 −0.7049 50.0005 34.7785 6.9923 50.0005 32.1119 −1.0988 50.0005 35.1839 6.3972 50.0005 32.5328 −1.4946 50.0005 35.5826 5.7972 50.0005 32.9526 −1.8932 50.0005 35.9755 5.1944 50.0005 33.3696 −2.2938 50.0005 36.3626 4.5877 50.0005 33.7847 −2.6964 50.0005 36.7439 3.9781 50.0005 34.1978 −3.1008 50.0005 37.1205 3.3657 50.0005 34.6090 −3.5072 50.0005 37.4912 2.7503 50.0005 35.0173 −3.9165 50.0005 37.8581 2.1311 50.0005 35.4246 −4.3267 50.0005 38.2192 1.5100 50.0005 35.8291 −4.7398 50.0005 38.5765 0.8860 50.0005 36.231.6 −5.1549 50.0005 38.9290 0.2590 50.0005 36.6322 −5.5709 50.0005 39.2776 −0.3698 50.0005 37.0309 −5.9898 50.0005 39.6223 −1.0015 50.0005 37.4277 −6.4097 50.0005 39.9632 −1.6352 50.0005 37.8225 −6.8324 50.0005 40.3012 −2.2717 50.0005 38.2154 −7.2571 50.0005 40.6354 −2.9082 50.0005 38.6054 −7.6828 50.0005 40.9676 −3.5477 50.0005 38.9935 −8.1122 50.0005 41.2979 −4.1871 50.0005 39.3768 −8.5456 50.0005 41.6253 −4.8284 50.0005 39.7571 −8.9818 50.0005 41.9528 −5.4688 50.0005 40.1337 −9.4219 50.0005 42.2792 −6.1111 50.0005 40.5054 −9.8649 50.0005 42.6047 −6.7525 50.0005 40.8732 −10.3108 50.0005 42.9302 −7.3948 50.0005 41.2363 −10.7605 50.0005 43.2547 −8.0371 50.0005 41.5955 −11.2121 50.0005 43.5792 −8.6804 50.0005 41.9499 −11.6686 50.0005 43.9019 −9.3237 50.0005 42.2985 −12.1289 50.0005 44.2245 −9.9670 50.0005 42.6432 −12.5921 50.0005 44.5451 −10.6112 50.0005 42.9832 −13.0582 50.0005 44.8639 −11.2574 50.0005 43.3202 −13.5262 50.0005 45.1788 −11.9045 50.0005 43.6544 −13.9971 50.0005 45.4879 −12.5545 50.0005 43.9866 −14.4690 50.0005 45.7922 −13.2074 50.0005 44.3150 −14.9437 50.0005 46.0927 −13.8613 50.0005 44.6414 −15.4204 50.0005 46.3883 −14.5181 50.0005 44.9640 −15.8990 50.0005 46.6801 −15.1758 50.0005 45.2837 −16.3795 50.0005 46.9671 −15.8354 50.0005 45.6006 −16.8639 50.0005 47.2511 −16.4970 50.0005 45.9135 −17.3493 50.0005 47.5304 −17.1605 50.0005 46.2217 −17.8385 50.0005 47.5863 −17.3059 50.0005 46.3113 −17.9723 50.0005 47.6412 −17.4725 50.0005 46.4201 −18.1168 50.0005 47.6864 −17.6420 50.0005 46.5366 −18.2554 50.0005 47.7201 −17.8154 50.0005 46.6637 −18.3845 50.0005 47.7374 −17.9906 50.0005 46.8014 −18.5010 50.0005 47.7297 −18.1659 50.0005 46.9555 −18.5954 50.0005 47.6874 −18.3373 50.0005 47.1269 −18.6541 50.0005 47.6036 −18.4904 50.0005 47.3070 −18.6628 50.0005 47.4765 −18.6060 50.0005 47.4765 −18.6060 50.0005 1.3241 15.3453 60.0002 1.3241 15.3453 60.0002 1.2442 16.0444 60.0002 1.6024 14.8310 60.0002 1.4214 16.7252 60.0002 2.0387 14.4410 60.0002 1.7421 17.3550 60.0002 2.5577 14.1704 60.0002 2.1465 17.9290 60.0002 3.1085 13.9836 60.0002 2.6087 18.4548 60.0002 3.6786 13.8603 60.0002 3.1153 18.9440 60.0002 4.2584 13.7872 60.0002 3.6536 19.3976 60.0002 4.8381 13.7525 60.0002 4.2179 19.8193 60.0002 5.4188 13.7544 60.0002 4.8024 20.2122 60.0002 6.0014 13.7852 60.0002 5.4005 20.5763 60.0002 6.5821 13.8064 60.0002 6.0120 20.9152 60.0002 7.1589 13.7958 60.0002 6.6360 21.2292 60.0002 7.7338 13.7621 60.0002 7.2725 21.5190 60.0002 8.3068 13.7111 60.0002 7.9216 21.7829 60.0002 8.8769 13.6398 60.0002 8.5841 22.0188 60.0002 9.4450 13.5483 60.0002 9.2553 22.2239 60.0002 10.0103 13.4376 60.0002 9.9313 22.3953 60.0002 10.5737 13.3066 60.0002 10.6131 22.5340 60.0002 11.1341 13.1574 60.0002 11.2988 22.6380 60.0002 11.6869 12.9908 60.0002 11.9912 22.7074 60.0002 12.2329 12.8088 60.0002 12.6874 22.7411 60.0002 12.7722 12.6113 60.0002 13.3904 22.7382 60.0002 13.3047 12.4005 60.0002 14.0934 22.6987 60.0002 13.8305 12.1741 60.0002 14.7867 22.6226 60.0002 14.3505 11.9363 60.0002 15.4724 22.5138 60.0002 14.8647 11.6849 60.0002 16.1494 22.3713 60.0002 15.3742 11.4230 60.0002 16.8187 22.1970 60.0002 15.8788 11.1486 60.0002 17.4812 21.9928 60.0002 16.3776 10.8645 60.0002 18.1351 21.7588 60.0002 16.8726 10.5708 60.0002 18.7832 21.4969 60.0002 17.3627 10.2665 60.0002 19.4226 21.2080 60.0002 17.8481 9.9554 60.0002 20.0505 20.8950 60.0002 18.3277 9.6357 60.0002 20.6648 20.5618 60.0002 18.8015 9.3112 60.0002 21.2667 20.2094 60.0002 19.2695 8.9799 60.0002 21.8570 19.8376 60.0002 19.7327 8.6429 60.0002 22.4368 19.4496 60.0002 20.1911 8.3010 60.0002 23.0059 19.0451 60.0002 20.6456 7.9553 60.0002 23.5654 18.6252 60.0002 21.0963 7.6038 60.0002 24.1162 18.1909 60.0002 21.5431 7.2494 60.0002 24.6555 17.7451 60.0002 21.9861 6.8902 60.0002 25.1842 17.2876 60.0002 22.4262 6.5281 60.0002 25.7023 16.8215 60.0002 22.8634 6.1622 60.0002 26.2107 16.3468 60.0002 23.2977 5.7934 60.0002 26.7096 15.8634 60.0002 23.7291 5.4216 60.0002 27.1997 15.3722 60.0002 24.1586 5.0470 60.0002 27.6822 14.8744 60.0002 24.5852 4.6705 60.0002 28.1560 14.3688 60.0002 25.0108 4.2921 60.0002 28.6221 13.8555 60.0002 25.4336 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90.0003 21.5287 19.8983 90.0003 17.2597 11.5106 90.0003 21.9716 19.4399 90.0003 17.6622 11.1187 90.0003 22.4088 18.9758 90.0003 18.0628 10.7248 90.0003 22.8383 18.5068 90.0003 18.4615 10.3291 90.0003 23.2630 18.0330 90.0003 18.8592 9.9323 90.0003 23.6809 17.5544 90.0003 19.2550 9.5336 90.0003 24.0931 17.0710 90.0003 19.6489 9.1330 90.0003 24.4995 16.5837 90.0003 20.0428 8.7315 90.0003 24.9020 16.0935 90.0003 20.4337 8.3289 90.0003 25.2997 15.5985 90.0003 20.8247 7.9254 90.0003 25.6926 15.0997 90.0003 21.2147 7.5200 90.0003 26.0807 14.5980 90.0003 21.6028 7.1136 90.0003 26.4659 14.0924 90.0003 21.9899 6.7072 90.0003 26.8463 13.5840 90.0003 22.3770 6.2989 90.0003 27.2228 13.0726 90.0003 22.7622 5.8897 90.0003 27.5955 12.5574 90.0003 23.1465 5.4794 90.0003 27.9643 12.0393 90.0003 23.5307 5.0682 90.0003 28.3293 11.5193 90.0003 23.9140 4.6570 90.0003 28.6904 10.9954 90.0003 24.2963 4.2449 90.0003 29.0487 10.4697 90.0003 24.6776 3.8317 90.0003 29.4030 9.9410 90.0003 25.0580 3.4177 90.0003 29.7536 9.4094 90.0003 25.4384 3.0026 90.0003 30.1012 8.8759 90.0003 25.8178 2.5876 90.0003 30.4440 8.3395 90.0003 26.1963 2.1715 90.0003 30.7849 7.8012 90.0003 26.5747 1.7555 90.0003 31.1220 7.2610 90.0003 26.9522 1.3386 90.0003 31.4552 6.7188 90.0003 27.3297 0.9206 90.0003 31.7855 6.1747 90.0003 27.7062 0.5027 90.0003 32.1119 5.6277 90.0003 28.0828 0.0838 90.0003 32.4355 5.0798 90.0003 28.4583 −0.3351 90.0003 32.7562 4.5299 90.0003 28.8329 −0.7550 90.0003 33.0740 3.9781 90.0003 29.2076 −1.1758 90.0003 33.3879 3.4244 90.0003 29.5812 −1.5966 90.0003 33.6989 2.8697 90.0003 29.9548 −2.0175 90.0003 34.0061 2.3121 90.0003 30.3275 −2.4393 90.0003 34.3104 1.7536 90.0003 30.6992 −2.8620 90.0003 34.6119 1.1931 90.0003 31.0700 −3.2848 90.0003 34.9104 0.6308 90.0003 31.4407 −3.7085 90.0003 35.2060 0.0674 90.0003 31.8105 −4.1322 90.0003 35.4978 −0.4988 90.0003 32.1793 −4.5578 90.0003 35.7867 −1.0660 90.0003 32.5482 −4.9825 90.0003 36.0727 −1.6342 90.0003 32.9160 −5.4082 90.0003 36.3558 −2.2043 90.0003 33.2820 −5.8348 90.0003 36.6380 −2.7763 90.0003 33.6469 −6.2633 90.0003 36.9173 −3.3483 90.0003 34.0090 −6.6938 90.0003 37.1946 −3.9213 90.0003 34.3692 −7.1261 90.0003 37.4710 −4.4943 90.0003 34.7255 −7.5605 90.0003 37.7464 −5.0682 90.0003 35.0799 −7.9967 90.0003 38.0209 −5.6431 90.0003 35.4314 −8.4358 90.0003 38.2953 −6.2180 90.0003 35.7800 −8.8769 90.0003 38.5678 −6.7929 90.0003 36.1257 −9.3198 90.0003 38.8413 −7.3679 90.0003 36.4685 −9.7657 90.0003 39.1139 −7.9437 90.0003 36.8085 −10.2145 90.0003 39.3854 −8.3196 90.0003 37.1445 −10.6642 90.0003 39.6551 −9.0964 90.0003 37.4797 −11.1168 90.0003 39.9218 −9.6742 90.0003 37.8138 −11.5694 90.0003 40.1847 −10.2549 90.0003 38.1480 −12.0220 90.0003 40.4418 −10.8366 90.0003 38.4812 −12.4756 90.0003 40.6932 −11.4211 90.0003 38.8144 −12.9291 90.0003 40.9397 −12.0085 90.0003 39.1476 −13.3827 90.0003 41.1814 −12.5969 90.0003 39.4788 −13.8363 90.0003 41.4183 −13.1872 90.0003 39.8111 −14.2918 90.0003 41.6523 −13.7795 90.0003 40.1423 −14.7463 90.0003 41.8796 −14.3736 90.0003 40.4717 −15.2028 90.0003 42.0982 −14.9716 90.0003 40.8010 −15.6592 90.0003 42.1444 −15.1103 90.0003 40.8925 −15.7786 90.0003 42.1897 −15.2682 90.0003 41.0023 −15.9086 90.0003 42.2272 −15.4281 90.0003 41.1188 −16.0319 90.0003 42.2542 −15.5908 90.0003 41.2430 −16.1475 90.0003 42.2667 −15.7555 90.0003 41.3769 −16.2515 90.0003 42.2561 −15.9212 90.0003 41.5252 −16.3343 90.0003 42.2137 −16.0800 90.0003 41.6870 −16.3834 90.0003 42.1338 −16.2226 90.0003 41.8565 −16.3863 90.0003 42.0154 −16.3314 90.0003 42.0154 −16.3314 90.0003 3.2048 27.3933 100.0000 3.2048 27.3933 100.0000 3.4735 27.9951 100.0000 3.1326 26.8347 100.0000 3.9049 28.4978 100.0000 3.2077 26.2772 100.0000 4.4413 28.8869 100.0000 3.4090 25.7494 100.0000 5.0307 29.1921 100.0000 3.6969 25.2641 100.0000 5.6354 29.4627 100.0000 4.0446 24.8231 100.0000 6.2527 29.7064 100.0000 4.4384 24.4234 100.0000 6.8806 29.9231 100.0000 4.8708 24.0613 100.0000 7.5162 30.1118 100.0000 5.3225 23.7195 100.0000 8.1575 30.2726 100.0000 5.7770 23.3815 100.0000 8.8027 30.4046 100.0000 6.2286 23.0425 100.0000 9.4518 30.5066 100.0000 6.6784 22.6987 100.0000 10.1047 30.5760 100.0000 7.1252 22.3520 100.0000 10.7634 30.6135 100.0000 7.5710 22.0034 100.0000 11.4259 30.6174 100.0000 8.0150 21.6529 100.0000 12.0865 30.5866 100.0000 8.4570 21.2995 100.0000 12.7413 30.5211 100.0000 8.8971 20.9441 100.0000 13.3885 30.4219 100.0000 9.3352 20.5859 100.0000 14.0279 30.2890 100.0000 9.7715 20.2257 100.0000 14.6606 30.1224 100.0000 10.2058 19.8627 100.0000 15.2865 29.9231 100.0000 10.6382 19.4987 100.0000 15.9029 29.6919 100.0000 11.0677 19.1308 100.0000 16.5086 29.4310 100.0000 11.4962 18.7620 100.0000 17.1008 29.1401 100.0000 11.9228 18.3903 100.0000 17.6796 28.8233 100.0000 12.3465 18.0166 100.0000 18.2420 28.4815 100.0000 12.7683 17.6411 100.0000 18.7899 28.1174 100.0000 13.1882 17.2626 100.0000 19.3224 27.7332 100.0000 13.6071 16.8832 100.0000 19.8415 27.3288 100.0000 14.0221 16.5009 100.0000 20.3480 26.9050 100.0000 14.4362 16.1166 100.0000 20.8411 26.4650 100.0000 14.8484 15.7305 100.0000 21.3206 26.0114 100.0000 15.2586 15.3414 100.0000 21.7867 25.5472 100.0000 15.6660 14.9505 100.0000 22.2384 25.0734 100.0000 16.0723 14.5576 100.0000 22.6785 24.5890 100.0000 16.4758 14.1627 100.0000 23.1060 24.0950 100.0000 16.8774 13.7660 100.0000 23.5240 23.5933 100.0000 17.2780 13.3673 100.0000 23.9313 23.0829 100.0000 17.6757 12.9657 100.0000 24.3310 22.5648 100.0000 18.0725 12.5632 100.0000 24.7210 22.0400 100.0000 18.4663 12.1578 100.0000 25.1042 21.5075 100.0000 18.8592 11.7514 100.0000 25.4788 20.9692 100.0000 19.2502 11.3421 100.0000 25.8467 20.4251 100.0000 19.6393 10.9319 100.0000 26.2069 19.8762 100.0000 20.0264 10.5197 100.0000 26.5593 19.3224 100.0000 20.4116 10.1056 100.0000 26.9060 18.7639 100.0000 20.7949 9.6906 100.0000 27.2459 18.2006 100.0000 21.1772 9.2727 100.0000 27.5801 17.6343 100.0000 21.5566 8.8538 100.0000 27.9075 17.0642 100.0000 21.9350 8.4339 100.0000 28.2301 16.4903 100.0000 22.3116 8.0121 100.0000 28.5469 15.9144 100.0000 22.6862 7.5884 100.0000 28.8580 15.3347 100.0000 23.0588 7.1637 100.0000 29.1642 14.7540 100.0000 23.4306 6.7371 100.0000 29.4666 14.1695 100.0000 23.7994 6.3095 100.0000 29.7632 13.5830 100.0000 24.1673 5.8810 100.0000 30.0569 12.9946 100.0000 24.5342 5.4505 100.0000 30.3458 12.4043 100.0000 24.8982 5.0191 100.0000 30.6309 11.8121 100.0000 25.2612 4.5858 100.0000 30.9120 11.2169 100.0000 25.6233 4.1515 100.0000 31.1894 10.6208 100.0000 25.9835 3.7152 100.0000 31.4648 10.0238 100.0000 26.3417 3.2790 100.0000 31.7354 9.4238 100.0000 26.6990 2.8408 100.0000 32.0041 8.8239 100.0000 27.0543 2.4007 100.0000 32.2689 8.2220 100.0000 27.4087 1.9607 100.0000 32.5318 7.6182 100.0000 27.7621 1.5186 100.0000 32.7918 7.0144 100.0000 28.1136 1.0757 100.0000 33.0489 6.4087 100.0000 28.4632 0.6317 100.0000 33.3032 5.8020 100.0000 28.8118 0.1859 100.0000 33.5545 5.1944 100.0000 29.1594 −0.2600 100.0000 33.8030 4.5858 100.0000 29.5051 −0.7078 100.0000 34.0495 3.9762 100.0000 29.8499 −1.1556 100.0000 34.2931 3.3647 100.0000 30.1937 −1.6043 100.0000 34.5348 2.7532 100.0000 30.5365 −2.0550 100.0000 34.7736 2.1407 100.0000 30.8774 −2.5057 100.0000 35.0105 1.5273 100.0000 31.2173 −2.9573 100.0000 35.2446 0.9120 100.0000 31.5563 −3.4090 100.0000 35.4776 0.2976 100.0000 31.8943 −3.8626 100.0000 35.7078 −0.3188 100.0000 32.2304 −4.3171 100.0000 35.9369 −0.9351 100.0000 32.5645 −4.7726 100.0000 36.1652 −1.5523 100.0000 32.8968 −5.2290 100.0000 36.3934 −2.1687 100.0000 33.2261 −5.6884 100.0000 36.6207 −2.7859 100.0000 33.5535 −6.1487 100.0000 36.8479 −3.4032 100.0000 33.8781 −6.6109 100.0000 37.0752 −4.0205 100.0000 34.1997 −7.0761 100.0000 37.3034 −4.6368 100.0000 34.5194 −7.5422 100.0000 37.5317 −5.2541 100.0000 34.8362 −8.0102 100.0000 37.7609 −5.8704 100.0000 35.1502 −8.4801 100.0000 37.9910 −6.4867 100.0000 35.4612 −8.9520 100.0000 38.2221 −7.1021 100.0000 35.7703 −9.4248 100.0000 38.4513 −7.7184 100.0000 36.0795 −9.8986 100.0000 38.6795 −8.3357 100.0000 36.3886 −10.3724 100.0000 38.9030 −8.9539 100.0000 36.6987 −10.8443 100.0000 39.1235 −9.5731 100.0000 37.0107 −11.3161 100.0000 39.3402 −10.1933 100.0000 37.3246 −11.7861 100.0000 39.5520 −10.8154 100.0000 37.6395 −12.2550 100.0000 39.7600 −11.4394 100.0000 37.9563 −12.7231 100.0000 39.9651 −12.0634 100.0000 38.2732 −13.1911 100.0000 40.1674 −12.6893 100.0000 38.5909 −13.6581 100.0000 40.3648 −13.3163 100.0000 38.9116 −14.1232 100.0000 40.5564 −13.9451 100.0000 39.2362 −14.5864 100.0000 40.5969 −14.0895 100.0000 39.3276 −14.7107 100.0000 40.6363 −14.2532 100.0000 39.4355 −14.8474 100.0000 40.6681 −14.4189 100.0000 39.5501 −14.9784 100.0000 40.6912 −14.5855 100.0000 39.6724 −15.1026 100.0000 40.7028 −14.7540 100.0000 39.8034 −15.2172 100.0000 40.6941 −14.9225 100.0000 39.9478 −15.3125 100.0000 40.6527 −15.0862 100.0000 40.1096 −15.3761 100.0000 40.5718 −15.2336 100.0000 40.2829 −15.3934 100.0000 40.4476 −15.3462 100.0000 40.4476 −15.3462 100.0000

TABLE II SUCTION-SIDE PRESSURE SIDE X (%) Y (%) Z (%) X (%) Y (%) Z (%) 52.5043 −16.7378 0.0000 51.2004 −17.4263 0.0000 52.5572 −16.8813 0.0000 51.2909 −17.5553 0.0000 52.6083 −17.0459 0.0000 51.3997 −17.6940 0.0000 52.6506 −17.2125 0.0000 51.5172 −17.8269 0.0000 52.6824 −17.3820 0.0000 51.6433 −17.9511 0.0000 52.6978 −17.5544 0.0000 51.7801 −18.0638 0.0000 52.6901 −17.7268 0.0000 51.9322 −18.1534 0.0000 52.6477 −17.8934 0.0000 52.0998 −18.2092 0.0000 52.5659 −18.0436 0.0000 52.2770 −18.2160 0.0000 52.4426 −18.1591 0.0000 52.4426 −18.1591 0.0000 51.6742 −17.1239 9.9997 50.3587 −17.7961 9.9997 51.7271 −17.2684 9.9997 50.4463 −17.9271 9.9997 51.7772 −17.4330 9.9997 50.5523 −18.0696 9.9997 51.8186 −17.6006 9.9997 50.6678 −18.2044 9.9997 51.8485 −17.7711 9.9997 50.7921 −18.3306 9.9997 51.8610 −17.9434 9.9997 50.9278 −18.4442 9.9997 51.8494 −18.1158 9.9997 51.0800 −18.5357 9.9997 51.8032 −18.2814 9.9997 51.2476 −18.5915 9.9997 51.7175 −18.4297 9.9997 51.4247 −18.5983 9.9997 51.5913 −18.5424 9.9997 51.5913 −18.5424 9.9997 50.7603 −17.3550 20.0004 49.4439 −18.0214 20.0004 50.8142 −17.4985 20.0004 49.5305 −18.1543 20.0004 50.8652 −17.6632 20.0004 49.6355 −18.2978 20.0004 50.9067 −17.8317 20.0004 49.7491 −18.4346 20.0004 50.9365 −18.0022 20.0004 49.8734 −18.5626 20.0004 50.9490 −18.1755 20.0004 50.0101 −18.6763 20.0004 50.9365 −18.3479 20.0004 50.1642 −18.7668 20.0004 50.8893 −18.5145 20.0004 50.3337 −18.8226 20.0004 50.8017 −18.6628 20.0004 50.5099 −18.8284 20.0004 50.6746 −18.7745 20.0004 50.6746 −18.7745 20.0004 49.7694 −17.4350 30.0001 48.4578 −18.1052 30.0001 49.8243 −17.5785 30.0001 48.5444 −18.2381 30.0001 49.8772 −17.7441 30.0001 48.6504 −18.3816 30.0001 49.9206 −17.9117 30.0001 48.7659 −18.5183 30.0001 49.9514 −18.0831 30.0001 48.8902 −18.6464 30.0001 49.9649 −18.2564 30.0001 49.0269 −18.7610 30.0001 49.9533 −18.4297 30.0001 49.1800 −18.8525 30.0001 49.9080 −18.5963 30.0001 49.3485 −18.9074 30.0001 49.8214 −18.7456 30.0001 49.5267 −18.9141 30.0001 49.6942 −18.8583 30.0001 49.6942 −18.8583 30.0001 48.6956 −17.3676 39.9998 47.3869 −18.0455 39.9998 48.7515 −17.5120 39.9998 47.4746 −18.1784 39.9998 48.8054 −17.6776 39.9998 47.5824 −18.3229 39.9998 48.8497 −17.8462 39.9998 47.6989 −18.4586 39.9998 48.8824 −18.0176 39.9998 47.8241 −18.5867 39.9998 48.8988 −18.1919 39.9998 47.9618 −18.7023 39.9998 48.8892 −18.3662 39.9998 48.1159 −18.7938 39.9998 48.8449 −18.5347 39.9998 48.2854 −18.8506 39.9998 48.7601 −18.6859 39.9998 48.4645 −18.8573 39.9998 48.6330 −18.8005 39.9998 48.6330 −18.8005 39.9998 47.5304 −17.1605 50.0005 46.2217 −17.8385 50.0005 47.5863 −17.3059 50.0005 46.3113 −17.9723 50.0005 47.6412 −17.4725 50.0005 46.4201 −18.1168 50.0005 47.6864 −17.6420 50.0005 46.5366 −18.2554 50.0005 47.7201 −17.8154 50.0005 46.6637 −18.3845 50.0005 47.7374 −17.9906 50.0005 46.8014 −18.5010 50.0005 47.7297 −18.1659 50.0005 46.9555 −18.5954 50.0005 47.6874 −18.3373 50.0005 47.1269 −18.6541 50.0005 47.6036 −18.4904 50.0005 47.3070 −18.6628 50.0005 47.4765 −18.6060 50.0005 47.4765 −18.6060 50.0005 46.2833 −16.8129 60.0002 44.9737 −17.4841 60.0002 46.3382 −16.9602 60.0002 45.0632 −17.6189 60.0002 46.3912 −17.1278 60.0002 45.1711 −17.7643 60.0002 46.4355 −17.2982 60.0002 45.2886 −17.9030 60.0002 46.4692 −17.4716 60.0002 45.4147 −18.0330 60.0002 46.4865 −17.6478 60.0002 45.5515 −18.1524 60.0002 46.4798 −17.8240 60.0002 45.7055 −18.2487 60.0002 46.4374 −17.9954 60.0002 45.8760 −18.3094 60.0002 46.3546 −18.1495 60.0002 46.0570 −18.3209 60.0002 46.2275 −18.2660 60.0002 46.2275 −18.2660 60.0002 44.9669 −16.3266 69.9999 43.6534 −16.9881 69.9999 45.0180 −16.4710 69.9999 43.7420 −17.1210 69.9999 45.0690 −16.6376 69.9999 43.8489 −17.2636 69.9999 45.1094 −16.8061 69.9999 43.9644 −17.4003 69.9999 45.1403 −16.9776 69.9999 44.0896 −17.5284 69.9999 45.1547 −17.1509 69.9999 44.2245 −17.6459 69.9999 45.1451 −17.3252 69.9999 44.3756 −17.7402 69.9999 45.1017 −17.4937 69.9999 44.5442 −17.7999 69.9999 45.0180 −17.6439 69.9999 44.7223 −17.8105 69.9999 44.8918 −17.7576 69.9999 44.8918 −17.7576 69.9999 43.5850 −15.7064 80.0006 42.2696 −16.3670 80.0006 43.6322 −15.8470 80.0006 42.3572 −16.4922 80.0006 43.6765 −16.0069 80.0006 42.4622 −16.6280 80.0006 43.7131 −16.1696 80.0006 42.5758 −163570 80.0006 43.7381 −16.3352 80.0006 42.6981 −16.8784 80.0006 43.7468 −16.5018 80.0006 42.8329 −16.9862 80.0006 43.7314 −16.6684 80.0006 42.9822 −17.0719 80.0006 43.6842 −16.8283 80.0006 43.1459 −17.1239 80.0006 43.5995 −16.9698 80.0006 43.3173 −17.1287 80.0006 43.4762 −17.0767 80.0006 43.4762 −17.0767 80.0006 42.0982 −14.9716 90.0003 40.8010 −15.6592 90.0003 42.1444 −15.1103 90.0003 40.8925 −15.7786 90.0003 42.1897 −15.2682 90.0003 41.0023 −15.9086 90.0003 42.2272 −15.4281 90.0003 41.1188 −16.0319 90.0003 42.2542 −15.5908 90.0003 41.2430 −16.1475 90.0003 42.2667 −15.7555 90.0003 41.3769 −16.2515 90.0003 42.2561 −15.9212 90.0003 41.5252 −16.3343 90.0003 42.2137 −16.0800 90.0003 41.6870 −16.3834 90.0003 42.1338 −16.2226 90.0003 41.8565 −16.3863 90.0003 42.0154 −16.3314 90.0003 42.0154 −16.3314 90.0003 40.5564 −13.9451 100.0000 39.2362 −14.5864 100.0000 40.5969 −14.0895 100.0000 39.3276 −14.7107 100.0000 40.6363 −14.2532 100.0000 39.4355 −14.8474 100.0000 40.6681 −14.4189 100.0000 39.5501 −14.9784 100.0000 40.6912 −14.5855 100.0000 39.6724 −15.1026 100.0000 40.7028 −14.7540 100.0000 39.8034 −15.2172 100.0000 40.6941 −14.9225 100.0000 39.9478 −15.3125 100.0000 40.6527 −15.0862 100.0000 40.1096 −15.3761 100.0000 40.5718 −15.2336 100.0000 40.2829 −15.3934 100.0000 40.4476 −15.3462 100.0000 40.4476 −15.3462 100.0000

It will also be appreciated that the airfoil 52 disclosed in the above Table I and the trailing edge profile 61 disclosed in Table II above may be scaled up or down geometrically for use in other similar turbine designs. Consequently, the coordinate values set forth in Table I or Table II may be scaled upwardly or downwardly such that the airfoil profile shape or trailing edge profile remains unchanged. A scaled version of the coordinates in Table I and/or Table II would be represented by X, Y and Z coordinate values of Table I and/or Table II, with the X. Y and Z non-dimensional coordinate values converted to units of distance (e.g., inches), multiplied or divided by a constant number.

An important term in this disclosure is “profile”. The profile is the range of the variation between measured points on an airfoil surface and the ideal position listed in Table I and Table II. The actual profile on a manufactured turbine rotor blade will be different than those in Table I, and the design is robust to this variation meaning that mechanical and aerodynamic function are not impaired. Similarly, the actual profile of the trailing edge on a manufactured turbine rotor blade will be different than those in Table II, and the design is robust to this variation meaning that mechanical and aerodynamic function are not impaired. As noted above, a + or −5% profile tolerance is used herein. The X, Y and Z values are all non-dimensionalized relative to the airfoil height.

The disclosed airfoil shape and the associated trailing edge profile optimizes and is specific to the machine conditions and specifications. It provides a unique profile to achieve 1) interaction between other stages in the turbine 10; 2) aerodynamic efficiency; and 3) normalized aerodynamic and mechanical blade loadings. The disclosed loci of points defined in Table I and/or Table II allow the gas turbine 12 or any other suitable turbine to run in an efficient, safe and smooth manner. As also noted, the disclosed airfoil 52 may be adapted to any scale, as long as 1) interaction between other stages in the pressure turbine 10; 2) aerodynamic efficiency; and 3) normalized aerodynamic and mechanical blade loadings are maintained in the scaled turbine.

The airfoil 52 described herein thus improves overall gas turbine 12 efficiency. Specifically, the airfoil 52 provides a desired turbine efficiency lapse rate (ISO, hot, cold, part load, etc.). The airfoil 52 also meets all aeromechanical and stress requirements. The turbine rotor blade 50 described herein has very specific aerodynamic design requirements, such as an upstream bucket radial back pressure (i.e., work splits) and radial velocity triangles for the downstream turbine rotors 150, 250, 350 and 450. Significant cross-functional design effort was required to meet these design goals. The airfoil 52 of the turbine rotor blade 50 thus is of a specific shape to meet aerodynamic, mechanical, and heat transfer requirements in an efficient and cost-effective manner.

This written description uses examples to disclose the invention, including the best mode, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims, if they have structural elements that do not differ from the literal language of the claims or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims. 

What is claimed is:
 1. A turbine rotor blade comprising an airfoil having an airfoil shape, the airfoil extending between a root and a tip and between a leading edge and a trailing edge, the airfoil shape having a nominal profile generally in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I the Cartesian coordinate values of X, Y, Z having a point data origin defined at the root at the leading edge of the airfoil, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a height of the airfoil in the unit of distance; and wherein X and Y values, when connected by continuing arcs, define airfoil profile sections at each Z value, the airfoil profile sections at Z values being joined with one another to form a complete airfoil shape.
 2. The turbine rotor blade of claim 1, wherein the turbine rotor blade forms part of a stage of a turbine.
 3. The turbine rotor blade of claim 1, wherein the turbine rotor blade is a second stage turbine rotor blade.
 4. The turbine rotor blade of claim 1, wherein the airfoil shape lies in an envelope within +/−5% of a chord length in a direction normal to any airfoil surface location.
 5. The turbine rotor blade of claim 1, wherein the height of the airfoil is about 5 inches to about 15 inches.
 6. The turbine rotor blade of claim 1, wherein the X, Y and Z values are scalable as a function of the same constant or number to provide a scaled-up or scaled-down airfoil.
 7. A turbine rotor blade comprising an airfoil having an uncoated nominal suction-side profile, the airfoil extending between a root and a tip and between a leading edge and a trailing edge, the uncoated nominal suction-side profile generally in accordance with suction-side Cartesian coordinate values of X, Y and Z set forth in Table I, the Cartesian coordinate values of X, Y, Z having a point data origin defined at the root at the leading edge of the airfoil, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a height of the airfoil in the unit of distance; and wherein X and Y values, when connected by continuing arcs, define suction-side profile sections at each Z value, the suction-side profile sections at the Z values being joined with one another to form a complete airfoil suction-side shape.
 8. The turbine rotor blade of claim 7, wherein the turbine rotor blade forms part of a stage of a turbine.
 9. The turbine rotor blade of claim 7, wherein the turbine rotor blade is a second stage turbine rotor blade.
 10. The turbine rotor blade of claim 7, wherein the suction-side shape lies in an envelope within +/−5% of a chord length in a direction normal to any airfoil surface location.
 11. The turbine rotor blade of claim 7, wherein the height of the airfoil is about 5 inches to about 15 inches.
 12. The turbine rotor blade of claim 7, wherein the X, Y and Z values are scalable as a function of the same constant or number to provide a scaled-up or scaled-down airfoil with the complete airfoil suction-side shape.
 13. A turbine rotor blade comprising an airfoil having an uncoated nominal trailing edge profile, the airfoil extending between a root and a tip and between a leading edge and a trailing edge, the uncoated nominal trailing edge profile generally in accordance with Cartesian coordinate values of X, Y and Z set forth in Table II, the Cartesian coordinate values of X, Y, Z having a point data origin defined at the root at the leading edge of the airfoil, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a height of the airfoil in the unit of distance; and wherein X and Y values, when connected by continuing arcs, define trailing edge profile sections at each Z value, the trailing edge profile sections at the Z values being joined with one another to form a complete trailing edge shape of the airfoil.
 14. The turbine rotor blade of claim 13, wherein the turbine rotor blade forms part of a stage of a turbine.
 15. The turbine rotor blade of claim 13, wherein the turbine rotor blade is a second stage turbine rotor blade.
 16. The turbine rotor blade of claim 13, wherein the trailing edge shape lies in an envelope within +/−5% of a chord length in a direction normal to any airfoil surface location.
 17. The turbine rotor blade of claim 13, wherein the height of the airfoil is about 5 inches to about 15 inches.
 18. The turbine rotor blade of claim 13, wherein the X, Y and Z values are scalable as a function of the same constant or number to provide a scaled-up or scaled-down airfoil with the nominal trailing edge profile.
 19. The turbine rotor blade of claim 13, wherein X represents a distance parallel to a turbine axis of rotation. 